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You searched for: publisher:"Washington, D.C. : NACA"
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[texts]Compression shocks in two-dimensional gas flows - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804321&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Shock waves
Downloads: 154
[texts]Formation of a vortex at the edge of a plate - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874042&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Gas flow
Downloads: 71
[texts]Heat transfer and pressure measurement on a 5-inch hemispherical concave nose at a Mach number of 2.0 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834297&ix=nu&I=0&V=D&pm=1
Keywords: Skin friction (Aerodynamics; Noses (Aircraft; Heat--Transmission
Downloads: 60
[texts]Nonstationary gas flow in thin pipes of variable cross section - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804176&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Difference equations; Gas flow
Downloads: 155
[texts]Review of the physical and thermodynamic properties of boric oxide - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853251&ix=nu&I=0&V=D&pm=1
Keywords: Thermodynamics--Research; Aerodynamics--Research
Downloads: 65
[texts]Concerning the flow about ring-shaped cowlings.: Part XII, two new classes of circular cowls - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003769345&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Radiators--Thermodynamics
Downloads: 54
[texts]On the problem of gas flow over an infinite cascade using Chaplygin's approximation - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874033&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Gas flow
Downloads: 72
[texts]Comparison of measured and predicted indicated angles of attack near the fuselages of a triangular-wing wind-tunnel model and a swept-wing fighter airplane in flight - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808552&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings, Triangular; Fighter planes--Wings--Testing; Aerodynamics--Research
Downloads: 71
[texts]Experimental investigation of air-flow uniformity and pressure level on wire cloth for transpiration-cooling applications - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810536&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Motors--Cooling; Aerodynamics--Research
Downloads: 100
[texts]Qualitative measurements of the effective heats of ablation of several materials in supersonic air jets at stagnation temperatures up to 11,000° F - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810791&ix=nu&I=0&V=D&pm=1
Keywords: Ablation (Aerothermodynamics; Supersonic planes; Aerodynamics--Research
Downloads: 91
[texts]Experimental determination of local and mean coefficients of heat transfer for turbulent flow in pipes - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778687&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Heat--Transmission
Downloads: 173
[texts]Concerning the flow about ring-shaped cowlings.: Part XIII, the influence of a projecting hub - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003769590&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Jet engines--Air intakes
Downloads: 87
[texts]Investigations on reductions of friction on wings, in particular by means of boundary layer suction - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875288&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Boundary layer--Research; Airplanes--Wings--Testing
Downloads: 106
[texts]Concerning the flow about ring-shaped cowlings.: Part VIII, further measurements on annular profiles - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779491&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Radiators--Thermodynamics
Downloads: 58
[texts]Contributions to the theory of the spreading of a free jet issuing from a nozzle - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779926&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Jet nozzles
Downloads: 58
[texts]Finite span wings in compressible flow - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807553&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings--Testing; Aerodynamics--Research
Downloads: 69
[texts]Report on the special field "interference" to the wind-tunnel committee in February 1945 - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003772597&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings; Drag (Aerodynamics
Downloads: 72
[texts]Autogenous welding in airplane construction - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874350&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Design and construction; Oxyacetylene welding and cutting
Downloads: 228
[texts]Approximate method for estimating the incompressible laminar boundary-layer characteristics on a flat plate in slipping flow - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810747&ix=nu&I=0&V=D&pm=1
Keywords: Laminar boundary layer; Aerodynamics--Research
Downloads: 71
[texts]Flow past a straight- and a swept-wing-body combination and their equivalent bodies of revolution at Mach numbers near 1.0 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808476&ix=nu&I=0&V=D&pm=1
Keywords: Body of revolution; Aerodynamics--Research
Downloads: 51
[texts]Generalization of Joukowski formula to an airfoil of a cascade in compressible gas stream with subsonic velocities - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779967&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Aerofoils
Downloads: 137
[texts]Gas flow with straight transition line - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003871226&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Gas flow
Downloads: 163
[texts]On the recording of turbulent longitudinal and transverse fluctuations - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779925&ix=nu&I=0&V=D&pm=1
Keywords: Buffeting (Aerodynamics; Turbulent boundary layer
Downloads: 60
[texts]Gas motion in a local supersonic region and conditions of potential-flow breakdown - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804207&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Supersonic planes
Downloads: 167
[texts]Effect of bluntness on the drag of spherical-tipped truncated cones of fineness ratio 3 at Mach numbers 1.2 to 7.4 - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810613&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Aerodynamics--Research
Downloads: 195
[texts]From linear mechanics to nonlinear mechanics - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874876&ix=nu&I=0&V=D&pm=1
Keywords: Remote control--Research; Nonlinear systems
Downloads: 104
[texts]Calculation of turbulent expansion processes - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780797&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Turbulent boundary layer
Downloads: 84
[texts]Experimental pressure distributions over two wing-body combinations at Mach number 1.9 - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810661&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings; Aerodynamics--Research
Downloads: 57
[texts]Theoretical analysis of stationary potential flows and boundary layers at high speed =: Theoretische untersuchungen über stationäre potentialströmungen und grenzschichten bei hohen geschwindigkeiten - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003604221&ix=nu&I=0&V=D&pm=1
Keywords: Gas dynamics; Laminar boundary layer; Aerodynamics--Research
Downloads: 73
[texts]Measurements of aerodynamic heat transfer and boundary-layer transition on a 10° cone in free flight at supersonic Mach numbers up to 5.9 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003854699&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research
Downloads: 55
[texts]Elasto-plastic stability of plates - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875399&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Elastic analysis (Engineering; Axial loads
Downloads: 61
[texts]Study of the flow over a 45° sweptback wing -fuselage combination at transonic Mach numbers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003809146&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics, Transonic; Airplanes--Wings, Swept-back; Aerodynamics--Research
Downloads: 70
[texts]General theory of conical flows and its application to supersonic aerodynamics - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778920&ix=nu&I=0&V=D&pm=1
Keywords: Superposition principle (Physics; Harmonic functions; Aerodynamics
Downloads: 201
[texts]On the representation of the stability region in oscillation problems with the aid of the Hurwitz determinants - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003771595&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Oscillations
Downloads: 176
[texts]Langley full-scale-tunnel tests of the custer channel wing airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808518&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 79
[texts]On rotational conical flow - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779475&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Rotational motion
Downloads: 153
[texts]Heat transfer and skin friction for turbulent boundary layers on heated or cooled surfaces at high speeds - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003809208&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics--Research; Skin friction (Aerodynamics
Downloads: 116
[texts]Nonlinear theory of a hot-wire anemometer - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778597&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings; Hot-wire anemometer
Downloads: 108
[texts]Concerning the flow about ring-shaped cowlings of finite thickness: Part I - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779497&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Motors--Cowlings
Downloads: 59
[texts]Effect of high viscosity on the flow around a cylinder and around a sphere - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779458&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Viscous flow
Downloads: 251
[texts]Investigation of Reynolds number effects for a series of cone-cylinder bodies at Mach number of 1.62, 1.93, and 2.41 - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808078&ix=nu&I=0&V=D&pm=1
Keywords: Skin friction (Aerodynamics; Aerodynamics--Research
Downloads: 88
[texts]Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003854698&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research
Downloads: 78
[texts]Remark on the theory of lifting surfaces - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807494&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings--Testing; Aerodynamics--Research
Downloads: 54
[texts]Approximate method for calculation of the laminar boundary layer with suction for bodies of arbitrary shape - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780854&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar boundary layer
Downloads: 83
[texts]Jet diffusion in proximity of a wall - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804195&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Jet engines
Downloads: 127
[texts]Resistance of cascade of airfoils in gas stream at subsonic velocity - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779974&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Aerodynamics; Laminar boundary layer
Downloads: 91
[texts]On the theory of the Laval nozzle - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804227&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Supersonic nozzles
Downloads: 196
[texts]Exploratory investigation of transpiration cooling of a 40° double wedge using nitrogen and helium as coolants at stagnation temperatures of 1,295° to 2,910° F - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853034&ix=nu&I=0&V=D&pm=1
Keywords: Transpiration (Physics; Aerodynamics--Research
Downloads: 49
[texts]On the instability of methods for the integration of ordinary differential equations - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875150&ix=nu&I=0&V=D&pm=1
Keywords: Numerical integration; Differential equations
Downloads: 72
[texts]Preliminary survey of possible cooling methods for hypersonic aircraft - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810781&ix=nu&I=0&V=D&pm=1
Keywords: Hypersonic planes; Airplanes--Motors--Cooling; Aerodynamics--Research
Downloads: 69
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